Parameter

4.7.3.10.2 natural laminar

Natural laminar flow refers to the phenomenon where airflow over an aircraft's surface remains laminar or smooth without the need for active flow control devices, resulting in reduced drag and improved fuel efficiency, typically achieved through careful shaping of the wing's surface contours, controlling the boundary layer behavior and maintaining a smooth surface finish.

Hierarchy

4 technological themes
4.1 active aircraft control
4.2 data transfer technologies
4.3 energy carriers
4.4 net zero technologies
4.5 operational technologies
4.6 aircraft propulsion
4.7 aircraft structures
4.7.1 aerospace materials & manufacturing
4.7.2 aircraft fuselage
4.7.3 aircraft wings
4.7.3.1 in-wing energy storage
4.7.3.2 morphing structures
4.7.3.3 wing smart structures
4.7.3.4 riblets
4.7.3.5 flow control (passive) on wings
4.7.3.6 high aspect ratio wing
4.7.3.7 foldable winglets
4.7.3.8 foldable wings
4.7.3.9 flexible skin
4.7.3.10 laminar wings
4.7.3.10.1 hybrid laminar
4.7.3.10.2 natural laminar
4.7.3.10.3 low sweep
4.7.3.11 prandtl plane
4.7.3.12 truss-braced wing
4.7.3.13 tube and wing optimization
4.7.3.14 wing bio-mimicry
4.7.3.15 passive load alleviation
4.7.3.16 wing structure as conductor
4.7.3.17 light/low mass paint/decals on wings
4.7.3.18 passive canards
4.7.3.19 in-flight cleaning of natural laminar flow leading edges
4.7.4 secondary structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
3
Optimising together
N/A
Stripping down
N/A
Tech for you
N/A
Mad max

Milestone Timehorizon

PESTEL categories

Current

Short term

Medium term

Long term

Little to many relations with other Milestones